NASA's Artemis II: Supercomputers to Wind Tunnels

5 Min Read

Of the many roads leading to successful Artemis missions, one is paved with high-tech computing chips called superchips. Along the way, a partnership between NASA wind tunnel engineers, data visualization scientists, and software developers verified a quick, cost-effective solution to improve NASA's SLS (Space Launch System) rocket for the upcoming Artemis II mission. This will be the first crewed flight of the SLS rocket and Orion spacecraft, on an approximately 10-day journey around the Moon.

A high-speed network connection between high-end computing resources at the NASA Advanced Supercomputing facility and the Unitary Plan Wind Tunnel, both located at NASA's Ames Research Center in California's Silicon Valley, is enabling a collaboration to improve the rocket for the Artemis II mission. During the Artemis I test flight, the SLS rocket experienced higher-than-expected vibrations near the solid rocket booster attach points, caused by unsteady airflow between the gap.

One solution proposed for Artemis II was adding four strakes. A strake is a thin, fin-like structure commonly used on aircraft to improve unsteady airflow and stability. Adding them to the core stage minimizes the vibration of components.

The strake solution comes from previous tests in the Unitary Plan Wind Tunnel, where NASA engineers applied an Unsteady Pressure Sensitive Paint (uPSP) technique to SLS models. The paint measures changes over time in aerodynamic pressures on air and spacecraft.

This supercomputer simulation peers down at a close-up of the SLS rocket during ascent. The force of friction is represented in greens, yellows, and blues. A six-foot-long strake flanking each booster's forward connection point on the SLS intertank smooths vibrations induced by airflow, represented by purples, yellows, and reds. The white streams represent a contour plot of density magnitude, highlighting the change of density in the air.

Credit: NASA/NAS/Gerrit-Daniel Stich, Michael Barad, Timothy Sandstrom, Derek Dalle

It is sprayed onto test models, and high-speed cameras capture video of the fluctuating brightness of the paint, which corresponds to the local pressure fluctuations on the model. Capturing rapid changes in pressure across large areas of the SLS model helps engineers understand the fast-changing environment. The data is streamed to the NASA Advanced Supercomputing facility via a high-speed network connection.

"This technique lets us see wind tunnel data in much finer detail than ever before. With that extra clarity, engineers can create more accurate models of how rockets and spacecraft respond to stress, helping design stronger, safer, and more efficient structures," said Thomas Steva, lead engineer, SLS sub-division in the Aerodynamics Branch at NASA's Marshall Space Flight Center in Huntsville, Alabama.

For the SLS configuration with the strakes, the wind tunnel team applied the paint to a scale model of the rocket. Once the camera data streamed to the supercomputing facility, a team of visualization and data analysis experts displayed the results on the hyperwall visualization system, giving the SLS team an unprecedented look at the effect of the strakes on the vehicle's performance. Teams were able to interact with and analyze the paint data.

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